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    • 65. 发明申请
    • MARINE PROPULSION SYSTEM
    • 海洋推进系统
    • US20110070782A1
    • 2011-03-24
    • US12993066
    • 2009-05-18
    • Codrin-Gruie CantemirGildo Pallanca
    • Codrin-Gruie CantemirGildo Pallanca
    • B63H11/14B63H21/38B63H11/10
    • B63H11/14B63H21/38B63H2011/002
    • A marine propulsion system comprising: a fuel-filled tank; an air compressor that generates compressed air; an engine that receives fuel from the tank, wherein the air compressor is powered by the engine; and at least one hot gas generator that receives compressed air from the air compressor, the hot gas generator comprising: (a) a combustion chamber having an inlet and an outlet, the compressed gas injected into the combustion chamber at the inlet, the combustion chamber adapted to produce hot gas; (b) an injection nozzle that receives fuel from the tank, the injection nozzle positioned proximate to the inlet of the combustion chamber, the injection nozzle adapted to spray the fuel into the combustion chamber; and (c) an exhaust nozzle positioned at the outlet of the combustion chamber through which the hot gas produced in the combustion chamber is discharged from the hot gas generator.
    • 一种船舶推进系统,包括:燃料填充罐; 产生压缩空气的空气压缩机; 从所述罐接收燃料的发动机,其中所述空气压缩机由所述发动机供电; 以及至少一个从空气压缩机接收压缩空气的热气体发生器,所述热气体发生器包括:(a)具有入口和出口的燃烧室,在入口处注入燃烧室的压缩气体,燃烧室 适应生产热气体; (b)喷嘴,其从所述罐接收燃料,所述喷嘴位于所述燃烧室的入口附近,所述喷嘴适于将所述燃料喷射到所述燃烧室中; 和(c)位于燃烧室出口处的排气喷嘴,燃烧室中产生的热气体通过该排气喷嘴从热气体发生器排出。
    • 67. 发明授权
    • High-speed watercraft
    • 高速船只
    • US5359958A
    • 1994-11-01
    • US239246
    • 1994-05-06
    • Johnithan R. Guild
    • Johnithan R. Guild
    • B63B1/16B63H11/14B63G1/16
    • B63H11/14B63B1/16
    • A high-speed watercraft provides a fast hydroplane craft, powered by a large gas turbine, that will plane over the surface of the water at high speed using a catamaran-type hull mounted on two long, flat-bottom pontoon skis with water chutes under the back end, with steering done from the front with a combination rudder/water chute. The turbine exhausts through a movable nozzle in the back that can be directed up or down by a hydraulic (or mechanical) actuator towards the surface of the water. The watercraft includes a large high, wide dual tail section having a tail wing and tail flap for control, and a large arch frame over the top from the front to the back with rods coming down to the gunnel to give the hull more strength. The craft also includes a front pontoon ski, a pair of middle pontoon skis, and a pair of aft pontoon skis. Finally, the craft includes a belly plate underneath near the back that acts like an after-ski with water chutes under the aft pontoon skis. Flat plates under the front of the skis mounted on pins. This will make the craft more stable to handle, less top heavy, better control, more floating buoyancy to skim over the surface of the water at high speeds and smoother riding.
    • 高速船只提供了一个快速的水上飞机,由一个大型燃气轮机提供动力,它将使用安装在两根长而平底的浮筒滑雪板上的双体船型船体高速平移在水面上,并配有水槽 后端,转向由前方组合舵/水槽。 涡轮机通过后面的可移动喷嘴排出,该喷嘴可以被液压(或机械)致动器向上或向下指向水表面。 船舶包括一个大的高,宽的双尾部分,具有用于控制的尾翼和尾翼,以及从前面到后面的顶部的大拱形框架,杆下降到枪口以给船体更多的力量。 该工艺还包括一个前悬浮式滑雪板,一对中型浮桥滑雪板和一对浮船滑雪板。 最后,这个工艺包括一个靠近后面的腹板,就像在浮船滑雪板下面的水滑道一样。 滑板前面的平板安装在销上。 这样可以使工艺更加稳定,更加重,更好的控制,更高的浮力,以更高的速度在水面上滑行,平稳的骑行。
    • 68. 发明授权
    • Liquid turbojet engine
    • 液体涡轮喷气发动机
    • US4897995A
    • 1990-02-06
    • US161156
    • 1988-02-26
    • Raafat H. Guirguis
    • Raafat H. Guirguis
    • B63H11/08B63H11/14
    • B63H11/14B63H11/08
    • A liquid turbojet engine includes an elongated shaft, a housing mounted about the shaft with the shaft being rotatable relative to the housing about the shaft longitudinal axis, a conduit fixed to the shaft within the housing filled with an inert motive liquid and nozzles for inducing combustible gas bubbles in the motive liquid. The conduit has a compression section extending generally radially from the shaft, a combustion section extending generally axially and parallel to the shaft and from the compression section at a radial distance from the shaft, and an expansion section extending generally radially relative to the shaft axis from an end of the combustion section remote from the compression section. The bubble nozzles are located at the inlet of the compression section. The motive liquid enters through an inlet in the housing. The burned bubbles are discharged with the motive liquid through an exit nozzle in the housing.
    • 液体涡轮喷气发动机包括细长轴,围绕轴安装的壳体,轴可相对于壳体围绕轴纵向轴线旋转,固定到壳体内的轴内的填充有惰性运动液体的导管和用于诱导可燃物的喷嘴 气泡在运动液体中。 导管具有从轴大体上径向延伸的压缩部分,大致轴向平行于轴并且与压缩部分相距一定距离地延伸的燃烧部分,以及相对于轴线从径向延伸的膨胀部分 燃烧部分的端部远离压缩部分。 气泡喷嘴位于压缩部分的入口处。 动力液体通过壳体中的入口进入。 燃烧的气泡通过动力液体通过壳体中的出口喷嘴排出。